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(2012 FS35)
Classification: Apollo [NEO]          SPK-ID: 3601672
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .118494600178526 5.04e-05  
a 1.098981994398325 5.0327e-05 au
q .9687585623686963 1.1042e-05 au
i 2.337391472202702 0.001563 deg
node 186.5251230960428 0.0012768 deg
peri 42.23021694171258 0.00078994 deg
M 2.087405740393302 0.18265 deg
tp 2458998.060006524057
(2020-May-28.56000652)
0.21333 TDB
period 420.8082953599394
1.15
0.028906
7.914e-05
d
yr
n .855496443320047 5.8765e-05 deg/d
Q 1.229205426427953 5.629e-05 au
  Orbit Determination Parameters
   # obs. used (total)      42  
   data-arc span      1 day  
   first obs. used      2012-03-25  
   last obs. used      2012-03-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .36463  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:50:20  

Additional Information
 Earth MOID = .000803885 au 
 Jupiter MOID = 3.74321 au 
 T_jup = 5.647 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456012.5 (2012-Mar-26.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1532019269930585 2.5685e-05  
q .9697151994808515 5.6266e-06 au
tp 2456048.279058416232
(2012-Apr-30.77905842)
0.0004935 TDB
node 5.490481676556601 1.4307e-05 deg
peri 218.8976082732661 0.0011158 deg
i 2.157047458872704 0.00033912 deg
  Orbit Determination Parameters
   # obs. used (total)      42  
   data-arc span      1 day  
   first obs. used      2012-03-25  
   last obs. used      2012-03-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .36463  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:50:20  

Additional Information
 Jupiter MOID = 3.74321 au 
 T_jup = 5.647 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.597237840086623E-10 -1.440700218515708E-10 1.090759963772773E-8 -3.242998692572318E-10 2.76982448094927E-8 8.445955142133916E-9
q -1.440700218515708E-10 3.165878791248037E-11 -2.492422931987112E-9 6.960341097086747E-11 -6.174528475548282E-9 -1.829022462815675E-9
tp 1.090759963772773E-8 -2.492422931987112E-9 2.435448427420732E-7 -4.852594204451373E-9 5.299558198266194E-7 1.334592205376225E-7
node -3.242998692572318E-10 6.960341097086747E-11 -4.852594204451373E-9 2.046932976796714E-10 -1.304952273781586E-8 -4.614873481347909E-9
peri 2.76982448094927E-8 -6.174528475548282E-9 5.299558198266194E-7 -1.304952273781586E-8 1.244945458383075E-6 3.475893500456399E-7
i 8.445955142133916E-9 -1.829022462815675E-9 1.334592205376225E-7 -4.614873481347909E-9 3.475893500456399E-7 1.150056064048232E-7

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 30.2   n/a MPO230291  

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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